CN206271985U - Anti-rotation buckle-type aviation plug - Google Patents
Anti-rotation buckle-type aviation plug Download PDFInfo
- Publication number
- CN206271985U CN206271985U CN201621453082.6U CN201621453082U CN206271985U CN 206271985 U CN206271985 U CN 206271985U CN 201621453082 U CN201621453082 U CN 201621453082U CN 206271985 U CN206271985 U CN 206271985U
- Authority
- CN
- China
- Prior art keywords
- rotation
- header body
- sleeve
- aviation plug
- jack body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model discloses a kind of anti-rotation buckle-type aviation plug, including header body and jack body, the header body front end is sleeve, the jack body and the sleeve that header body inserted terminal is that outer wall is provided with helicla flute, the sleeve inner side of the header body front end is provided with quantity and helicla flute quantity identical pin, and anti-rotation device is additionally provided between the jack body and header body；Anti-rotation device is installed between the jack body and header body of existing buckle-type aviation plug, on the premise of the quick connection of buckle-type aviation plug and separating property is played, effectively prevents from being come off in vibration environment, improve connective stability；Anti-rotation device is formed using serrated slot and anti-rotation switch combination in the utility model, after jack body and header body are screwed, anti-rotation switch front end is located in serrated slot, anti-rotation switch can only be axially moved in serrated slot, prevent the automatic reverse rotation in vibration environment of jack body and header body, it is ensured that be stably connected with.
Description
Technical field
The utility model is related to aviation plug technical field, more particularly to a kind of anti-rotation buckle-type aviation plug.
Background technology
Aviation plug is typically made up of plug and socket, and wherein plug is also referred to as free endAviation plug, socket is also referred to as fixationAviation plug.Plug together and separate and realize being connected and disconnected from for circuit by plug, socket, therefore just generate plug and insert
The various connected modes of seat.For circular aviation plug, mainly there are screw-type connection, bayonet coupling and cylinder type connection three
The mode of kind.Wherein screw-type connection is most common, it have processing technology it is simple,Manufacturing costLow, applied widely the advantages of, but
Connection speed is unsuitable for frequently plugging more slowly and quick a sequence of occasion.Buckle-type connects leading due to its three helicla flutes
Journey is more long, therefore the speed for connecting, but it manufactures more complicated, and cost is also just higher.Cylinder type connection is three kinds of connection sides
Most fast one kind of connection speed in formula, it is not required to be rotated, and need to only carry outLinear motionCan be achieved with connecting, separate and
The function of locking, but find in use, and buckle-type aviation plug easily comes off in frequent vibration environment, makes
Into Joint failure, therefore, a kind of relatively reliable buckle-type aviation plug of connection of exploitation design is that asking for solution is badly in need of in this area
Topic.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of anti-rotation buckle-type aviation plug, in existing buckle
Anti-rotation device is installed between the jack body and header body of formula aviation plug, is quickly connected buckle-type aviation plug is played
On the premise of separating property, effectively prevent from being come off in vibration environment, improve connective stability.
In order to solve the above technical problems, technical solution adopted in the utility model is：A kind of anti-rotation buckle-type aviation
Plug, including header body and jack body, the header body front end are sleeve, the jack body and header body grafting
The sleeve that helicla flute is provided with for outer wall is held, it is identical with helicla flute quantity to be provided with quantity on the inside of the sleeve of the header body front end
Pin, be additionally provided with anti-rotation device between the jack body and header body.
The anti-rotation device includes the serrated slot being located on jack body outer wall and is symmetrically mounted on header body front end
Two sets of anti-rotation switches of sleeve ends, serrated slot is uniform around jack body axis, and the anti-rotation switch is relative to plug sheet
The axisymmetrical of body front end sleeve installs two sets, and anti-rotation switch is L-shaped platy structure, right on the plug head sleeve outer wall
Claim to set two mounting seats, the anti-rotation switch is joined by means of pin and mounting seat and installs torsion spring between mounting seat,
The plug head sleeve lateral wall is provided with the breach for accommodating anti-rotation switch.
The anti-rotation micro- end of switch is provided with the pressure hand being upturned.
It is using the beneficial effect produced by above-mentioned technical proposal：Existing buckle-type aviation plug jack body with
Anti-rotation device is installed between header body, on the premise of the quick connection of buckle-type aviation plug and separating property is played, is had
Effect prevents from being come off in vibration environment, improves connective stability；Serrated slot and anti-rotation switch combination are used in the utility model
Anti-rotation device is formed, after jack body and header body are screwed, anti-rotation switch front end is located in serrated slot, anti-rotation switch
Can only be axially moved in serrated slot, prevent the automatic reverse rotation in vibration environment of jack body and header body, it is ensured that steady
Fixed connection.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is jack body and header body exploded view；
Wherein：1st, header body；2nd, anti-rotation switch；3rd, jack body；4th, serrated slot；5th, mounting seat；6th, helicla flute.
Specific embodiment
With reference to the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out clearly
Chu, it is fully described by, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of the utility model protection.
Many details are elaborated in the following description in order to fully understand the utility model, but this practicality is new
Type can also be different from other manner described here using other be implemented, and those skilled in the art can be without prejudice to this reality
Similar popularization is done with the case of new intension, therefore the utility model is not limited by following public specific embodiment.
As shown in Figure 1-2, the utility model discloses a kind of anti-rotation buckle-type aviation plug, including the He of header body 1
Jack body 3, the front end of the header body 1 is sleeve, and the jack body 3 is with the inserted terminal of header body 1 for outer wall is provided with
The sleeve of helicla flute 6, the sleeve inner side of the front end of the header body 1 is provided with quantity and the quantity identical pin of helicla flute 6, described
Anti-rotation device is additionally provided between jack body 3 and header body 1.
Before the anti-rotation device includes the serrated slot 4 being located on the outer wall of jack body 3 and is symmetrically mounted on header body 1
The anti-rotation switch 2 in end two sets of sleeve ends, serrated slot 4 is uniform around the axis of jack body 3, it is described it is anti-rotation switch 2 relative to
The axisymmetrical of the front end sleeve of header body 1 installs two sets, and anti-rotation switch 2 is L-shaped platy structure, the plug head sleeve
Be symmetrical arranged two mounting seats 5 on outer wall, the anti-rotation switch 2 joined by means of pin and mounting seat 5 and with mounting seat 5
Between torsion spring is installed, the plug head sleeve lateral wall is provided with the breach for accommodating anti-rotation switch 2；It is described anti-rotation to open
Close 2 micro- ends and be provided with the pressure hand being upturned.
During concrete application, when header body 1 is screwed with jack body 3, traveller edge in the front end sleeve of header body 1
Helicla flute 6 turns clockwise and in axial direction advances on jack body, after anti-rotation switch contact is to serrated slot 4, plug
Body is not rotatable, can only advance along serrated slot 4, until header body is screwed with jack body, header body and jack body
Engagement is finished.
When header body is separated with jack body, hold header body simultaneously press anti-rotation switch, make it is anti-rotation switch with
Serrated slot is separated, rotate counterclockwise header body, makes in header body cylinder along the direction rotate counterclockwise of serrated slot 4, and along axle
Draw back, until departing from jack body.
In a word, the utility model installs anti-rotation between the jack body and header body of existing buckle-type aviation plug
Device, on the premise of the quick connection of buckle-type aviation plug and separating property is played, effectively prevents from being come off in vibration environment,
Improve connective stability；Anti-rotation device, jack body are formed using serrated slot and anti-rotation switch combination in the utility model
After being screwed with header body, anti-rotation switch front end is located in serrated slot, and anti-rotation switch can only be axially moved in serrated slot,
Prevent the automatic reverse rotation in vibration environment of jack body and header body, it is ensured that be stably connected with.
Claims (3)
1. a kind of anti-rotation buckle-type aviation plug, including header body（1）And jack body（3）, the header body（1）Before
It is sleeve to hold, the jack body（3）With header body（1）Inserted terminal is provided with helicla flute for outer wall（6）Sleeve, it is described insert
Head body（1）The sleeve inner side of front end is provided with quantity and helicla flute（6）Quantity identical pin, it is characterised in that：The socket
Body（3）With header body（1）Between be additionally provided with anti-rotation device.
2. anti-rotation buckle-type aviation plug according to claim 1, it is characterised in that：The anti-rotation device includes setting
In jack body（3）Serrated slot on outer wall（4）Be symmetrically mounted on header body（1）Two sets of front end sleeve ends are anti-rotation
Switch（2）, serrated slot（4）Around jack body（3）Axis is uniform, the anti-rotation switch（2）Relative to header body（1）Front end
The axisymmetrical of sleeve installs two sets, anti-rotation switch（2）It is L-shaped platy structure, it is symmetrical on the plug head sleeve outer wall
Two mounting seats are set（5）, the anti-rotation switch（2）By means of pin and mounting seat（5）Handing-over and and mounting seat（5）It
Between torsion spring is installed, the plug head sleeve lateral wall is provided with for accommodating anti-rotation switch（2）Breach.
3. anti-rotation buckle-type aviation plug according to claim 2, it is characterised in that：The anti-rotation switch（2）It is micro-
End is provided with the pressure hand being upturned.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621453082.6U CN206271985U (en) | 2016-12-28 | 2016-12-28 | Anti-rotation buckle-type aviation plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621453082.6U CN206271985U (en) | 2016-12-28 | 2016-12-28 | Anti-rotation buckle-type aviation plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206271985U true CN206271985U (en) | 2017-06-20 |
Family
ID=59047601
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621453082.6U Expired - Fee Related CN206271985U (en) | 2016-12-28 | 2016-12-28 | Anti-rotation buckle-type aviation plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206271985U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107230890A (en) * | 2017-06-28 | 2017-10-03 | 陈柯 | A kind of sanding apparatus |
| CN107871978A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of electricity consumption with electroshock-proof function plugs together component |
| CN107871992A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of Novel electric plugs together component |
| CN107871979A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of modified electricity consumption plugs together component |
-
2016
- 2016-12-28 CN CN201621453082.6U patent/CN206271985U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107230890A (en) * | 2017-06-28 | 2017-10-03 | 陈柯 | A kind of sanding apparatus |
| CN107871978A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of electricity consumption with electroshock-proof function plugs together component |
| CN107871992A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of Novel electric plugs together component |
| CN107871979A (en) * | 2017-06-28 | 2018-04-03 | 徐学铖 | A kind of modified electricity consumption plugs together component |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170620 Termination date: 20171228 |